|Publication number||US6792184 B2|
|Application number||US 10/411,406|
|Publication date||Sep 14, 2004|
|Filing date||Apr 10, 2003|
|Priority date||May 31, 2002|
|Also published as||CN1781047A, CN100430767C, US7085459, US20030223714, US20040223709, WO2004092778A2, WO2004092778A3|
|Publication number||10411406, 411406, US 6792184 B2, US 6792184B2, US-B2-6792184, US6792184 B2, US6792184B2|
|Inventors||Craig M. Conrad, David W. Chiasson, Bradley J. Blazer, Eric R. Logan|
|Original Assignee||Corning Cable Systems Llc|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (36), Non-Patent Citations (3), Referenced by (12), Classifications (6), Legal Events (6)|
|External Links: USPTO, USPTO Assignment, Espacenet|
The present application is a Continuation-In-Part (CIP) of U.S. Ser. No. 10/159,730 filed on May 31, 2002, the disclosure of which is incorporated herein by reference.
The present invention relates generally to fiber optic ribbons. More specifically, the invention relates to fiber optic ribbons having a preferential separation sequence for tearing the fiber optic ribbon.
Fiber optic ribbons include optical waveguides such as optical fibers that transmit optical signals, for example, voice, video, and/or data information. Fiber optic cables using optical fiber ribbons can result in a relatively high optical fiber-density. Fiber optic ribbon configurations can be generally classified into two general categories. Namely, fiber optic ribbons with subunits and those without. A fiber optic ribbon with a subunit configuration, for example, includes at least one optical fiber surrounded by a primary matrix forming a first subunit, and a second subunit having a similar construction, which are contacted and/or encapsulated by a secondary matrix. On the other hand, fiber optic ribbons without subunits generally have a plurality of optical fibers surrounded by a single layer of matrix material.
Optical fiber ribbons should not be confused with micro-cables that, for example, have a strength member and a jacket. For instance, U.S. Pat. No. 5,673,352 discloses a micro-cable having a core structure and a jacket. The core structure requires that at least one optical fiber is positioned between longitudinally extending strength members, both of which are embedded in a buffer material. The jacket protects the core structure and the material is selected to have good adhesion to the buffer material and be abrasion resistant. Additionally, the strength members are required to have a larger diameter than the diameter of the optical fiber, thereby absorbing crushing forces that are applied to the cable.
On the other hand, optical fiber ribbons generally have a plurality of adjacent optical fibers arranged in a generally planar array forming a relatively high optical fiber density. Optical fiber ribbons without subunits can present problems for the craft. For example, when separating these optical fiber ribbons into optical fiber subsets, the craft must use expensive precision tools. Moreover, connectorization/splice procedures can require inventories of specialized splice and closure units/tools for the various subsets of optical fibers. Where the craft elects to separate the optical fiber ribbon into subsets by hand, or with a tool lacking adequate precision, stray optical fibers and/or damage to the optical fibers can result. Stray optical fibers can cause problems in optical ribbon connectorization, organization, stripping, and splicing. Additionally, damage to the optical fibers is undesirable and can render the optical fiber inoperable for its intended purpose.
However, there are fiber optic ribbon configurations that attempt to aid the separation of fiber optic ribbons without using subunits. For example, U.S. Pat. No. 5,982,968 requires an optical fiber ribbon of uniform thickness having V-shaped stress concentrations in the matrix material that extend along the longitudinal axis of the fiber optic ribbon. V-shaped stress concentrations can be located across from each other on the planar surfaces of the fiber optic ribbon, thereby aiding the separation of the fiber optic ribbon into subsets. However, the '968 patent requires a wider fiber optic ribbon because additional matrix material is required adjacent to the optical fibers near the V-shaped stress concentrations to avoid stray optical fibers after separation. A wider ribbon requires more matrix material and decreases the optical fiber density. Another embodiment of the patent requires applying a thin layer of a first matrix material around optical fibers to improve geometry control such as planarity of the optical fibers. Then V-shaped stress concentrations are formed in a second matrix applied over the first matrix material, thereby allowing separation of the subsets at the stress concentrations.
Another example of a separable fiber optic ribbon is described in U.S. Pat. No. 5,970,196. More specifically, the '196 patent requires a pair of removable sections positioned in V-shaped notches located across from each other on opposite sides of the planar surfaces of an optical fiber ribbon. The removable sections are positioned between adjacent interior optical fibers of the optical fiber ribbon to facilitate the separation of the optical fiber ribbon into subsets at the V-shaped notches. The removable sections can either be flush with the planar surfaces of the optical fiber ribbon, or they may protrude therefrom. These known fiber optic ribbons have several disadvantages. For example, they can be more expensive and difficult to manufacture. Additionally, from an operability standpoint, the V-shaped stress concentrations and/or V-shaped notches can undesirably affect the robustness of the optical fiber ribbon and/or induce microbending in the optical fibers.
Fiber optic ribbons that employ subunits to aid separation generally do not encounter these problems; however, they-can have other problems. A conventional optical fiber ribbon 1 employing subunits encapsulated in a secondary matrix is shown in FIG. 1. Optical fiber ribbons having subunits can have several advantages, for example, improved separation, and avoidance of stray fiber occurrences. In particular, optical fiber ribbon 1 includes a pair of conventional subunits 2 having optical fibers 3 encapsulated in a primary matrix 5, which are then encapsulated in a secondary matrix 4. The thickness T1 of primary matrix 5 is continuous and uniform. Likewise, the thickness t1 of the secondary matrix 4 covering the planar portions of subunits 2 is continuous and uniform. For example, subunit 2 can include six 250 μm optical fibers 3 disposed in primary matrix 5 having an overall uniform thickness T1 of 310 μm and secondary matrix 4 has a thickness t1 of 10 μm for an overall fiber optic ribbon thickness T2 of 330 μm.
However, conventional optical fiber ribbon 1 has disadvantages. For example, one concern is the potential formation of wings W (FIG. 1) during hand separation of subunits 2. Wings W can be cause by, for example, a lack of sufficient adhesion between common matrix 4 and subunit matrix 5 and/or random fracturing of the secondary matrix during separation. The existence of wings W can negatively affect, for example, optical ribbon organization, connectorization, stripping, and/or splicing operations by the craft. Additionally, wings W can cause problems with ribbon identification markings, or compatibility of the subunit with ribbon handling tools, for example, thermal strippers, splice chucks, and fusion splicers.
The present invention is directed to a fiber optic ribbon having a predetermined separation sequence including, a first subunit, a second subunit, and a secondary matrix. The first and second subunits each have a respective plurality of optical fibers arranged in a generally planar configuration being connected by respective first and second primary matricies. The first subunit is a portion of a first ribbon-unit and second subunit is a portion of a second ribbon-unit that includes a plurality of subunits. The secondary matrix connects the first ribbon-unit and the second ribbon-unit so that the secondary matrix has a preferential tear portion disposed adjacent to a ribbon-unit interface defined between the first ribbon-unit and the second ribbon-unit.
The present invention is also directed to a fiber optic ribbon having a predetermined separation sequence including a first subunit, a second subunit, and a secondary matrix. The first and second subunits have a respective plurality of optical fibers arranged in a generally planar configuration being connected by respective first and second primary matricies having a non-uniform thickness. The first subunit is a portion of a first ribbon-unit and the second subunit is a portion of a second ribbon-unit that includes a plurality of subunits. A ribbon interface is formed between the first subunit and the second subunit and the secondary matrix connects the first ribbon-unit and the second ribbon-unit. The secondary matrix has at least one local minimum thickness adjacent to the ribbon-unit interface so that the secondary matrix fractures at the ribbon interface before fracturing at a subunit interface of one of the ribbon-units.
The present invention is further directed to a fiber optic ribbon including a first subunit, a second subunit, and a secondary matrix. The first and second subunits including respective pluralities of optical fibers being contacted by respective first and second primary matricies. The first subunit is a portion of a first ribbon-unit and the second subunit is a portion of a second ribbon-unit having at least two subunits. The first and second ribbon-units are generally aligned along a plane. The secondary matrix has a cross-section with a non-uniform thickness that contacts portions of the first and second subunits. The secondary matrix also has at least one recessed portion defining at least a portion of a preferential tear portion. The at least one recessed portion being adjacent to a ribbon-unit interface defined between the first ribbon-unit the second ribbon-unit.
Additionally, the present invention is directed to a fiber optic ribbon having a predetermined separation sequence including a first secondary matrix, a second secondary matrix, and a tertiary matrix. The first secondary matrix connecting at least a first subunit and a second subunit together, thereby forming a first ribbon-unit, wherein the first and second subunits respectively include a plurality of optical fibers arranged in a generally planar configuration being connected by a respective primary matrix. The second secondary matrix connecting at least a third subunit and a fourth subunit together, thereby forming a second ribbon-unit, wherein the third and fourth subunits respectively include a plurality of optical fibers arranged in a generally planar configuration being connected by a respective primary matricies. The tertiary matrix connects the first ribbon-unit and the second ribbon-unit. The tertiary matrix has a preferential tear portion at an interface between the first ribbon-unit and the second ribbon-unit.
FIG. 1 is a cross-sectional view of a conventional optical fiber ribbon according to the background of the present invention.
FIG. 2 is a cross-sectional view of a fiber optic ribbon according to one embodiment of the present invention.
FIG. 3 is a cross-sectional view of another fiber optic ribbon according to the present invention.
FIG. 3a is a partial cross-sectional view of other fiber optic ribbons according to the present invention.
FIG. 4 is a cross-sectional view of the fiber optic ribbon subunit of FIG. 2 having a secondary matrix on portions thereof.
FIG. 5 is a cross-sectional view of another fiber optic ribbon according to the present invention.
FIG. 6 is a cross-sectional view of the fiber optic ribbon of FIG. 5 after separation into subunits.
FIG. 7 is a cross-sectional view of another fiber optic ribbon according to the present invention.
FIG. 8 is a cross-sectional view of another fiber optic ribbon according to the present invention.
FIG. 9 is a cross-sectional view of another fiber optic ribbon according to the present invention.
FIG. 10 is a schematic, partial cross-sectional view of another fiber optic ribbon according to the present invention.
FIG. 11 is a cross-sectional view of a fiber optic ribbon having a preferential separation sequence according to the present invention.
FIG. 12 is a cross-sectional view of another fiber optic ribbon having a preferential separation sequence according to the present invention.
FIG. 13 is a cross-sectional view of a fiber optic ribbon having a preferential separation sequence according to the present invention.
FIG. 14 is a cross-sectional view of a fiber optic cable according to the present invention.
Illustrated in FIG. 2 is a fiber optic ribbon 10 according to the present invention. Fiber optic ribbon 10 (hereinafter ribbon) includes a plurality of optical waveguides, for example, optical fibers 12 arranged in a generally planar configuration with a primary matrix 14 forming an elongate structure. Ribbon 10 can, for example, be used as a stand-alone ribbon, a portion of a ribbon stack, or as a subunit of a ribbon. Primary matrix 14 generally contacts optical fibers 12 and may encapsulate the same, thereby providing a robust structure for processing and handling. Primary matrix 14 generally fixes adjacent optical fibers together in an elongate structure, thereby inhibiting relative movement therebetween. Primary matrix 14 includes a first end 14 a, a medial portion 14 b, and a second end 14 c. Additionally, primary matrix 14 has a cross-section having a non-uniform thickness.
In this embodiment, first end portion 14 a has a thickness Ta and second end portion 14 c has a thickness Tc, which are both greater than a thickness Tb of medial portion 14 b. For example, thickness Ta is about 5 μm or greater than thickness Tb; however, other suitable dimensions can be used. More particularly, first and second end portions 14 a, 14 c both have a generally bulbous shape; however, other suitable shapes can be used such as angular or elliptical. As used herein, bulbous shape means that an end portion of the ribbon has a thickness that is greater than the largest thickness of a medial portion of the ribbon. Preferably, the largest thickness is generally adjacent to edge fiber 12 a, generally at a range r of about one-half to about one optical fiber diameter from the edge of the matrix, however, other suitable ranges can be used. Suitable values of range r generally dispose the largest thickness Ta over a cross-section of edge fiber 12 a. In other words, range r is between a point tangent to a circumference of the edge fiber 12 a (shown by dashed line on left ribbon of FIG. 3A) to a point over edge fiber 12 a (shown by right ribbon of FIG. 3A) up to about one optical fiber diameter or more inward from the edge of the matrix.
The present invention should not be confused with conventional ribbons having undulations across their cross-sections surfaces due to manufacturing variances. These undulations can cause variations in the conventional ribbon thickness at random locations, rather than, for example, predetermined shapes. For example, the thickness of the conventional ribbon can be 310±3 μm at random locations across the cross-section. On the other hand, ribbons according to the present invention can have, for example, a non-uniform thickness that increases or decreases at predetermined locations to aid separation performance.
In one embodiment, optical fibers 12 are a plurality of single-mode optical fibers; however, other types or configurations of optical fibers can be used. For example, optical fibers 12 can be multi-mode, pure-mode, erbium doped, polarization-maintaining fiber, other suitable types of light waveguides, and/or combinations thereof. For instance, each optical fiber 12 can include a silica-based core that is operative to transmit light and is surrounded by a silica-based cladding having a lower index of refraction than the core. Additionally, one or more coatings can be applied to optical fiber 12. For example, a soft primary coating surrounds the cladding, and a relatively rigid secondary coating surrounds the primary coating. The coating can also include an identifying means such as ink or other suitable indicia for identification and/or an anti-adhesion agent that inhibits the removal of the identifying means. However, optical fibers used in ribbons of the present invention generally are not tight-buffered. Suitable optical fibers are commercially available from Corning Incorporated of Corning, N.Y.
Primary matrix 14 can be, for example, a radiation curable material or a polymeric material; however, other suitable materials can be used. As known to one skilled in the art, radiation curable materials undergo a transition from a liquid to a solid when irradiated with predetermined radiation wavelengths. Before curing, the radiation curable material includes a mixture of formulations of, for example, liquid monomers, oligomer “backbones” with acrylate functional groups, photoinitiators, and other additives. Typical photoinitiators function by: absorbing energy radiated by the radiation source; fragmenting into reactive species; and then initiating a polymerization/hardening reaction of the monomers and oligomers. Generally, as a result of irradiation, a cured solid network of cross-linking is formed between the monomers and oligomers, which may include fugitive components. Stated another way, the photoinitiator begins a chemical reaction that promotes the solidification of the liquid matrix into a generally solid film having modulus characteristics.
One aspect of the curing process is the reaction of a photoinitiator in response to radiation exposure. A photoinitiator has an inherent absorption spectrum that is measured in terms of absorbance as a function of radiation wavelength. Each photoinitiator has a characteristic photoactive region, i.e., a photoactive wavelength range typically measured in nanometers (nm). For example, commercially available photoinitiators can have a photoactive wavelength range in the vacuum ultra-violet (160-220 nm), ultra-violet (220-400 nm), or visible light (400-700 nm) wavelength ranges.
The resulting modulus of radiation curable materials can be controlled by factors such as radiation intensity and cure time. The radiation dose, i.e., the radiant energy arriving at a surface per unit area is inversely proportional to the line speed, i.e., the speed the radiation curable moves past the radiation source. The light dose is the integral of radiated power as a function of time. In other words, all else being equal, the faster the line speed, the higher the radiation intensity must be to achieve adequate curing. After a radiation curable material has been fully irradiated, the material is said to be cured. Curing occurs in the radiation curable material from the side facing the radiation source down or away from the source. Because portions of the material closer to the radiation source can block radiation from reaching non-cured portions of the material, a cure gradient can be established. Depending on the amount of incident radiation, a cured material may exhibit different degrees of curing. Moreover, the degrees of curing in a material can have distinct modulus characteristic associated therewith. Conversely, radiation sources can be positioned so that the material has a relatively uniform cure.
Thus, the degree of cure affects the mechanical characteristics through the cross-link density of the radiation curable material. For example, a significantly cured material can be defined as one with a high cross-link density for that material, which is, for example, too brittle. Further, an undercured material may be defined as one having a low cross-link density, and can be too soft, possibly having a relatively high coefficient of friction (COF) that causes an undesirable level of ribbon friction. The cured UV material has a modulus, for example, in the range of about 50 MPa to about 1500 MPa depending on the radiation dose. Different modulus values can provide varying degrees of performance with respect to, for example, hand separability and robustness of the ribbons of the present invention.
In one embodiment, a UV curable material is used for primary matrix 14. For example, the UV curable material is a polyurethane acrylate resin commercially available from DSM Desotech Inc. of Elgin Ill. such as 950-706. Alternatively, other suitable UV materials can be used, for example, polyester acrylate resin commercially available from Borden Chemical, Inc. of Columbus, Ohio. Additionally, thermoplastic materials such as polypropylene can be used as a matrix material.
FIG. 3 illustrates a ribbon 20 another embodiment of the present invention that is similar to ribbon 10. Ribbon 20 includes a plurality of optical waveguides, for example, optical fibers 12 arranged in a generally planar configuration with a primary matrix 24 forming an elongate structure. Primary matrix 24 generally contacts optical fibers 12 and may encapsulate the same, thereby providing a robust structure for processing and handling. Primary matrix 24 includes a cross-section having a non-uniform thickness having a first end 24 a, a medial portion 24 b, and a second end 24 c. In this embodiment, first end portion 24 a has a thickness Ta and second end portion 24 c has a thickness Tc, wherein thickness Ta is greater than a thickness Tb of medial portion 24 b. More particularly, first end portion 24 a, for example, has a generally bulbous shape; however, other suitable shapes can be used. Whereas, second end portion 24 c can have a shape that is generally different than the shape of first end portion 24 a. For example, as depicted, second end portion 24 c has a generally round shape, however, other suitable shapes can be used such as flat, angled, radiused, or combinations thereof. When stacking a plurality of ribbons similar to ribbon 20, first end portion 24 a can be placed on alternating sides of the ribbon stack to provide stack integrity. Additionally, stacking ribbons in this manner still allows the ribbons to move in at least two degrees of freedom when acted upon by forces, which can preserve optical performance.
FIG. 3a depicts a plurality of ribbons 30 having a primary matrix 34 with a non-uniform cross-sectional thickness having thickness Ta disposed over a cross-section of the edge optical fiber. Specifically, an end portions 34 a is formed from several shapes such as linear and radius portions, thereby forming a generally angular end portion that is bulbous. Preferably, a medial portion 34 b has a thickness Tb that extends over, or past, a diameter D of edge optical fiber 12 a. By extending thickness Tb over, or past, diameter D of edge optical fiber 12 a the planarity of the optical fibers of ribbon 30, particularly edge optical fiber 12 a, is easier to control. Additionally, end portion 34 a includes a predetermined angle α that can influence the amount of secondary matrix disposed between adjacent ribbons 30 when they are used as subunits for larger ribbons. In other words, angle α can influence performance parameters such as twist performance and separation characteristics when ribbons 30 are used as subunits by tailoring the amount of secondary matrix therebetween. Additionally, other suitable shapes can be used.
FIG. 4 depicts a ribbon 40. Ribbon 40 includes ribbon 10 with a secondary matrix 45 disposed on outwardly portions of primary matrix 14. Using more than one can have several advantages. For example, in one embodiment a thin primary matrix can be applied to ensure planarity of the optical fibers in the; ribbon. Additionally, secondary matrix 45 can have several functions. For example, secondary matrix 45 can be used impart generally planar surfaces 46 to ribbon 40. Planar surfaces 46 can also provide stability when ribbon 40 is used as a portion of a ribbon stack. Additionally, secondary matrix 45 may also provide material characteristics that are different from primary matrix 14 such as adhesion, COF characteristics, or hardness. This can be accomplished, for example, by using a secondary matrix 45 material that is similar to primary matrix 14 with different processing characteristics such as cure characteristics, or by using a material that is different than primary matrix 14. Likewise, different portions of secondary matrix 45 can be different materials and/or have distinct material characteristics.
Illustratively, a first planar surface of secondary matrix 45 can have a predetermined COF, while the second planar surface can have a high adhesion to primary matrix 14. A predetermined COF on the planar surface allows the ribbon to relieve strain, for example, during bending of a stack of ribbons. While a high adhesion characteristic between the primary and secondary matrices can make for a generally robust ribbon. In other embodiments, the first and second planar surfaces can have the same characteristics, which may differ from the characteristics of the primary matrix. Additionally, as disclosed in U.S. Pat. No. 6,253,013, which is incorporated in its entirety herein by reference, an adhesion zone 44 (FIG. 4) can be used between primary matrix 14 and secondary matrix 45. For example, adhesion zone 44 is applied to primary matrix 14 using a Corona discharge treatment. Additionally, a marking indicia for identifying ribbon 40 can be printed either on primary matrix 14 or secondary matrix 45. In other embodiments, secondary matrix 45 can be used to identify ribbon 40. For example, secondary matrix 45 can be colored with a dye for identification of the ribbon.
Likewise, other suitable color combinations are possible for identifying individual ribbons. In one embodiment, primary matrix 14 may be a first color and secondary matrix 45 a second color. For example, multiple ribbons of a ribbon stack can have the same color primary matrix with each different ribbon have a secondary matrix with a different color. Thus, the craftsman could identify the stack as the blue stack and each individual ribbon within the blue stack. In other embodiments, the secondary matrix of the ribbons of the stack can be the same color, with the primary matrix of the individual ribbon having different colors. Thus, each ribbon can be identified from the side of the stack. In still other embodiments, the primary or secondary matrix can have stripes, or tracers, of suitable colors for use as identifying indicia.
FIG. 5 depicts ribbon 50 another embodiment according to the present invention. Ribbon 50 includes two ribbons such as ribbons 10 for use as a first subunit 51 and a second subunit 52. As used herein, subunit means a plurality of optical fibers having a discrete matrix material thereon. In other words, each subunit has its own individual matrix material thereon. Subunits should not be confused with subsets, which are optical fibers arranged as groups having a common matrix material. When subunits are separated, the discrete matrix material generally remains intact on each subunit. However, ribbons according to the present invention can use other suitable types or numbers of ribbons as subunits.
A secondary matrix 55 contacts portions of subunits 51, 52 and is generally dimensioned to provide a pair of opposing generally flat planar surfaces 56. Secondary matrix 55 can have material characteristics that are similar or different than the primary matrix. For example, the primary and/or the secondary matrix around the edge fibers of subunits 51, 52 can be relatively soft to cushion the same and inhibit optical attenuation therein. The generally flat planar surfaces 56 allow ribbon 50 to be easily stacked to form a portion of a ribbon stack. However, other suitable shapes of secondary matrix 55 can be used. Using secondary matrix 55 allows separation of ribbon 50 at the interface 57 between the subunits 51, 52 by, for example, hand. Subunits 51, 52 preferably have a point of contact at interface 57, thereby allowing secondary matrix 55 to flow between the subunits and forming a robust structure. However, the subunits can be spaced apart at the interface therebetween.
Additionally, ribbon 50 advantageously inhibits the formation of, for example, wings and/or stray optical fibers during separation. Ribbon 50 inhibits the formation of wings by having a preferential tear portion 58 in secondary matrix 55, rather than allowing random fracturing in secondary matrix 55. Specifically, preferential tear portion 58 is generally located at a point of local minimum thickness t2 (FIG. 6) and is generally adjacent to interface 57 of secondary matrix. In this case, the local minimum thickness t2 is formed by subunits 51, 52 having non-uniform cross-sections. When secondary matrix 55 with generally flat planar surfaces 56 is applied over these non-uniform cross-sections, the thickness of secondary matrix 55 varies. For example, local minimum thickness t2 is about 2 μm, whereas portions of the secondary matrix 55 over the medial portions of subunits 51, 52 have a thickness of about 10 μm. In other embodiments, local minimum thickness t2 can approach a value of essentially zero. Local minimum thickness t2 is a weak point, thereby allowing the fracture of secondary matrix 55 to begin and/or terminate at this point. Additionally, the minimum thickness can have other suitable dimensions or locations, but should allow the ribbon to have a suitable robustness and handleability. FIG. 6 illustrates the ribbon 50 after separation by hand into subunits. As depicted, formation of wings is inhibited according to the concepts of the present invention. Additionally, using suitable matrix characteristics such as elongation to break and/or a predetermined matrix modulus can enhance the preferential tear portion.
As depicted in FIG. 7, preferential tear portion can be accomplished with other suitable ribbon geometries. Ribbon 70 includes two subunits 71, 72 and a secondary matrix 75. Secondary matrix 75 contacts and/or encapsulates subunits 71, 72 thereby forming ribbon 70. Like secondary matrix 55 of ribbon 50, secondary matrix 75 has a thickness that varies generally adjacent to interface 77 between subunits 71, 72. However, the varying thickness of secondary matrix 75 adjacent interface 77 is accomplished with subunits 71, 72 having a generally uniform thickness. However, this ribbon configuration can be used in combination with subunits having a non-uniform thickness. In one embodiment, secondary matrix 75 has a recessed portion having a width w, for example, the recessed portion defining a concave portion 73 generally centered over interface 77. In other words, recessed portions are generally symmetrical about an interface axis A—A that passes through interface 77 and is generally perpendicular to the generally planar surfaces of ribbon 70. However, in other embodiments, the recessed portion can have other shapes such as indentation 74, widths, and/or locations. For purposes of illustration, the top and bottom of ribbon 70 have different configurations of the recessed portion; however, embodiments can have the same shaped recessed portions 73 on each side of interface 77. Concave portions 73 form a local minimum thickness in secondary matrix 75, which is a weak point that advantageously allows the fracture of secondary matrix 75 to begin and/or terminate at this point during, for example, hand separation.
In one embodiment, recessed portion 73 has a width w less than about 600 μm and a depth D of about 5 μm. However, other suitable dimensions can be used, for example, in other embodiments width w can be about 200 μm or greater and depth D can be about 5 μm or greater. Furthermore, the recessed portions 73 of the ribbon should be dimensioned to provide suitable robustness and handleability for the intended application of the ribbon.
Ribbon 80, another embodiment according to the concepts of the present invention, is illustrated in FIG. 8. Ribbon 80 includes a pair of subunits 81, 82, each having a generally uniform thickness, and a secondary matrix 85 generally contacting and/or encapsulating subunits 81, 82, thereby forming ribbon 80. Ribbon 80 has at least one recessed portion 83 and is similar to ribbon 70; however, recessed portions 83 are centered over an interface 87 between subunits 81, 82. In this embodiment, recessed portions 83 have a generally concave shape that is offset at a distance d from interface 87. For example, distance d is between about 125 μm and about 300 μm, but other suitable distances can be used. Additionally, recessed portions 83 can have other shapes, widths, and/or depths. For purposes of illustration, the top and bottom of ribbon 80 have a different number of recessed portions 83. For example, recessed portions 83 on the top of ribbon 80 are generally symmetrical about interface axis A—A. However, other embodiments can have the same, or different, number of recessed portions 83 on each generally planar surface 86, for example, one, two, or more. Concave portions 83 form a local minimum thickness in secondary matrix 85, which is a weak point that advantageously allows the fracture of secondary matrix 75 to begin and/or terminate at this point during, for example, hand separation, thereby inhibiting the formation of wings.
Recessed portions 83 should be dimensioned to provide suitable robustness and handleability for the intended application of the ribbon. In this embodiment, centering recessed portions 83 of ribbon 80 at distance d from interface 87 provides increased robustness to ribbon 80. Specifically, centering recessed portions 83 from interface 87 improves the twist performance of ribbon 80. For example, subunits 81, 82 of ribbon 80 are less likely to separate during normal handling of the ribbon.
FIG. 9 illustrates a ribbon 90 that is another embodiment of the present invention that is similar to ribbon 50. Ribbon 90 includes subunits 91, 92 and a secondary matrix 95. Secondary matrix 95 contacts and/or encapsulates subunits 91, 92 thereby forming ribbon 90. Subunits 91, 92 have a non-uniform thickness and secondary matrix 95 has a plurality of recessed portions, like ribbon 70. In this embodiment, recessed portions 83 are on both sides of interface axis A—A and are generally symmetrical thereabout. The recessed portions are defined as a plurality of concave portions 93; however, recessed portions can have other shapes, widths, and/or locations. Concave portions 93 are generally located at a distance d from the interface of subunits 91, 92. In this embodiment, distance d locates the center of concave portions 93 slightly beyond the largest thickness of the ends towards the medial portions of the subunits 91, 92.
FIG. 10 illustrates a portion of ribbon 100, which is another embodiment that is similar to ribbon 90. Ribbon 100 includes subunits 101, 102 and a secondary matrix 105. Subunits 101, 102 have a non-uniform thickness and secondary matrix 105 has plurality of recessed portions that are symmetrical about interface axis A—A, thereby forming a local minimum thickness t2. In this embodiment, local minimum thickness t2 is formed by having a radius R1 of the subunit being less than an adjacent radius R2 of the primary matrix, thereby forming a preferential tear portion. For example, local minimum thickness t2 can have a range of about zero to about 5 μm; however, any other suitable dimension can be used. Radii R1 and R2 are generally located adjacent to local minimum thickness t2. Configuring the ribbon so that R2 is greater than R1, is intended to allow secondary matrix 105 material to generally flow away from local minimum thickness t2 before curing or hardening of the same. In other words, radius R1 and the surface tension of secondary matrix 105 cause matrix 105 to flow away, thereby forming the local minimum thickness, rather than having primary matrix material flow towards, and building-up the thickness of local minimum thickness t2. Additionally, other embodiments can also use this concept.
FIG. 11 illustrates ribbon 110 including a secondary matrix 115 having a plurality of preferential tear portions 115 a, 115 b for separating a plurality of ribbon-units A, B, and C, thereby providing ribbon 110 with a preferential separation sequence. In other words, ribbon 110 has a preference to separate at a ribbon-unit interface(s) A/B and/or B/C before separating at a subunit interface such as between subunits 112, 113. In this embodiment, each subunit 111-114 includes two optical fibers 12 that are connected by respective primary matrcies (not numbered) having a generally uniform thickness. Each ribbon-unit A, B, and C includes at least one subunit, but at least one of the ribbon-units should include at least two subunits. In this case, ribbon-unit B includes two subunits 112, 113 having two optical fibers and ribbon-units A and C each include one subunit having two optical fibers. The preferential separation sequence occurs at the ribbon-unit interfaces A/B and/or B/C because the preferential tear portions 115 a, 115 b of secondary matrix 115 are disposed adjacent to respective ribbon-unit interfaces. On the other hand, secondary matrix 115 has a generally uniform thickness adjacent to the subunit interface between subunits 112, 113, thereby creating a more robust connection between the subunit interface compared with the ribbon-unit interface. Preferential tear portions 115 a are recessed portions and preferential tear portion 115 b is an indentation. However, ribbons of the present invention can include any suitable preferential tear portion or feature to provide the preferential separation sequence of the ribbon-units. For instance, other embodiments of ribbon 110 can have asymmetrical forms such as two ribbon-units A and B respectively having one and two subunits with a minimum of six optical fibers in the ribbon. Additionally, ribbon-units can include other suitable numbers of subunits and/or subunits can include suitable numbers of optical fibers.
Furthermore, the concepts of a preferential separation sequence between ribbon-units can employ subunits having other suitable geometry. For instance, FIG. 12 depicts ribbon 120 having ribbon-units E,F,G with respective subunits that can include a non-uniform thickness connected by a secondary matrix 127 having preferential tear portions. In this case, subunits 122-126 have at least a first end portion with a thickness that is greater than a medial portion and subunit 121 is a subunit with a generally uniform thickness. Preferably, a first and a second end of subunits are generally symmetrical so that orientation during ribbonizing is of no concern; however, end portions can have different shapes so that orientation during ribbonizing matters. Moreover, having generally symmetrical subunits with non-uniform thicknesses can inhibit the formation of wings during separation of subunits in the same ribbon-unit if necessary. As depicted, subunits 122, 123, 124 have at least one end portions with a generally angular shape and subunits 124, 125, 126 have at least one end portions with a generally bulbous shape.
As shown, secondary matrix 127 includes at least one preferential tear portion disposed adjacent to ribbon interfaces E/F and F/G. Specifically, preferential tear portions of secondary matrix are recessed portions 127 a having a generally concave shape that is offset at a distance d from the ribbon-unit interface. For example, distance d is between about 125 μm and about 300 μm, but other suitable distances can be used. Additionally, recessed portions 127 a can have other shapes, widths, and/or depths. Additionally, the top and bottom of ribbon 120 can have different numbers or shapes of recessed portions 127 a. In this case, recessed portions 127 a are generally symmetrical about axis A—A at the ribbon-unit interface.
Still further, the concepts of a preferential separation sequence between ribbon-units can employ more than two matrices. For instance, FIG. 13 depicts ribbon 130 having ribbon-units H, I, J connected by a tertiatry matrix having preferential tear portions. Specifically, the subunits of ribbon 130 include optical fibers connected by respective primary matricies (not numbered) and each ribbon-unit H, I, J includes two subunits connected by a respective secondary matrix 137 that are connected by a tertiary matrix 138. Tertiary matrix 138 includes preferential tear portions such as recesses 138 a or indentations; however, any suitable preferential tear portion as described herein can be used. Additionally, any of the matrices can include the material characteristics, properties and/or features as discussed herein.
Moreover, the ribbons of the present invention can be used in any suitable fiber optic cable design. FIG. 14 depicts a representative fiber optic cable 140 according to the present invention. Fiber optic cable 140 includes a stack 142 of ribbons 110 disposed in a tube 144 having a sheath 146 therearound. Sheath 146 includes strength members 146 a and a jacket 146 b. Although a monotube fiber optic cable design is depicted, the present invention can include the ribbons of the present invention in any suitable cable design such as dry-tube, slotted core, drop cables, figure-eight, loose tube, or interconnect cables. Moreover, fiber optic cable 140, or any other cable configuration, can include more, or fewer, cables components such as ripcords, armor layers, binder layers, strength members, tubeless, water-swellable components, water-blocking materials, or any other suitable cable components.
Many modifications and other embodiments of the present invention, within the scope of the appended claims, will become apparent to a skilled artisan. For example, subunits can include different numbers of optical fibers, ribbons can have more than two subunits, or the ribbons can have other suitable configurations. Additionally, ribbons of the present invention can have suitable components such as ripcords. Therefore, it is to be understood that the invention is not to be limited to the specific embodiments disclosed herein and that modifications and other embodiments may be made within the scope of the appended claims. Although specific terms are employed herein, they are used in a generic and descriptive sense only and not for purposes of limitation. The invention has been described with reference to silica-based optical fibers, but the inventive concepts of the present invention are applicable to other suitable optical waveguides as well.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US4547040||Jun 21, 1983||Oct 15, 1985||Mitsubishi Rayon Co., Ltd.||Optical fiber assembly and process for preparing same|
|US4653852||Jan 3, 1985||Mar 31, 1987||Sumitomo Electric Industries, Ltd||Multi core optical fiber|
|US4752112||Feb 24, 1987||Jun 21, 1988||Siemens Aktiengesellschaft||Ribbon conductor comprising a plurality of light waveguides and a method of manufacture|
|US4861135||Feb 16, 1988||Aug 29, 1989||Kabelmetal Electro Gesellschaft Mit Beschrankter Haftung||Ribbon cable with optical waveguides|
|US4900126||Jun 30, 1988||Feb 13, 1990||American Telephone & Telegraph Co.||Bonded array of transmission media|
|US5442722||Jul 25, 1994||Aug 15, 1995||Siecor Corporation||Optical fiber ribbon with zip cord|
|US5457762||Jun 13, 1994||Oct 10, 1995||Siecor Corporation||Fiber optic ribbon|
|US5524164||Jan 13, 1994||Jun 4, 1996||Sumitomo Electric Industries, Ltd.||Coated tape form optical fiber wire|
|US5598498||Sep 30, 1994||Jan 28, 1997||Alcatel Cavi S.P.A.||Modular optical fiber core tape, separable into a plurality of tape units or modules, method of manufacturing such tape and optical cable using the same|
|US5673352||Jan 12, 1996||Sep 30, 1997||Alcatel Submarine Networks, Inc.||Fiber optic micro cable|
|US5717805||Jun 12, 1996||Feb 10, 1998||Alcatel Na Cable Systems, Inc.||Stress concentrations in an optical fiber ribbon to facilitate separation of ribbon matrix material|
|US5761363||Mar 7, 1996||Jun 2, 1998||Siecor Corporation||Optical fiber ribbon which is strippable and peelable|
|US5905835||Jul 31, 1997||May 18, 1999||Alcatel Cable France||Optical fiber multi-ribbon|
|US5933559||Jan 22, 1998||Aug 3, 1999||Dsm N.V.||Radiation-curable cross-linked ribbon matrix material for bonding an array of coated optical glass fibers|
|US5970196||Sep 22, 1997||Oct 19, 1999||Siecor Corporation||Fiber optic protective member with removable section to facilitate separation thereof|
|US5982968||Feb 9, 1998||Nov 9, 1999||Alcatel Na Cable System, Inc.||Stress concentrations in an optical fiber ribbon to facilitate separation of ribbon matrix material|
|US6018605||Dec 31, 1997||Jan 25, 2000||Siecor Operations||Photoinitiator--tuned optical fiber and optical fiber ribbon and method of making the same|
|US6028976||Nov 18, 1997||Feb 22, 2000||Sumitomo Electric Industries, Ltd.||Split type ribbon optical fiber core cable|
|US6097866||May 1, 1998||Aug 1, 2000||Alcatel||Optical fiber ribbon|
|US6253013||Mar 29, 1999||Jun 26, 2001||Siecor Operations, Llc||Optical fiber arrays|
|US6309567||Jun 24, 1999||Oct 30, 2001||Sumitomo Electric Industries, Ltd.||Collectively coating die device for manufacturing separable optical fiber ribbon and manufacturing method thereof|
|US6337941||Sep 29, 1999||Jan 8, 2002||Alcatel||Splittable optical fiber ribbons|
|US6381390||Apr 6, 1999||Apr 30, 2002||Alcatel||Color-coded optical fiber ribbon and die for making the same|
|EP0843187A1||Nov 17, 1997||May 20, 1998||Sumitomo Electric Industries, Ltd.||Split type ribbon optical fiber core cable|
|EP0856761A1||Jan 30, 1998||Aug 5, 1998||Fujikura Ltd.||Optical fiber cord, ribbon cord using the same and ribbon cord branch line|
|JPH01138517A||Title not available|
|JPH01138518A||Title not available|
|JPH01251005A||Title not available|
|JPH07120645A||Title not available|
|JPH08129122A||Title not available|
|JPH08262292A||Title not available|
|JPH09113773A||Title not available|
|JPH09197213A||Title not available|
|JPH09218328A||Title not available|
|WO1994023323A1||Mar 30, 1994||Oct 13, 1994||Nokia Kaapeli Oy||Optical fibre ribbon|
|WO1997005515A1||Jul 31, 1996||Feb 13, 1997||Dsm Nv||A ribbon unit, a method of making the ribbon unit and a method of providing mid-span access|
|1||N. Andrew Punch, Jr., Shail K. Moorjani, Steven T. Bissell, and Karen E. Williams, Craft-Friendly 24-Fiber Ribbon Design, IWCS 1999, pp. 72-78.|
|2||R. S. Wagman, G. A. Lochkovic, K. T. White, "Component Optimization for Slotted Core Cables Using 8-Fiber Ribbons", IWCS 1995, pp. 472-478.|
|3||U.S. patent application Publication 2002/025128A1, Feb. 28, 2002, Hwang.|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US7187830||Dec 22, 2004||Mar 6, 2007||Corning Cable Systems, Llc.||Optical fiber ribbons having a preferential tear portion formed by curing and methods therefor|
|US7206481||Dec 21, 2004||Apr 17, 2007||Corning Cable Systems, Llc.||Fiber optic cables manufactured as an assembly and method for manufacturing the same|
|US7415181||Jul 29, 2005||Aug 19, 2008||Corning Cable Systems Llc||Fiber optic cables and assemblies for fiber to the subscriber applications|
|US7465879||Apr 21, 2006||Dec 16, 2008||Cable Components Group||Concentric-eccentric high performance, multi-media communications cables and cable support-separators utilizing roll-up designs|
|US7473849||Apr 21, 2006||Jan 6, 2009||Cable Components Group||Variable diameter conduit tubes for high performance, multi-media communication cable|
|US7473850||Apr 21, 2006||Jan 6, 2009||Cable Components Group||High performance, multi-media cable support-separator facilitating insertion and removal of conductive media|
|US7532796||Sep 29, 2006||May 12, 2009||Corning Cable Systems Llc||Fiber optic ribbons having one or more predetermined fracture regions|
|US7787727||Sep 3, 2009||Aug 31, 2010||Corning Cable Systems Llc||Dry fiber optic cables and assemblies|
|US8467647||Dec 11, 2007||Jun 18, 2013||Prysmian Communication Cables And Systems Usa, Llc||Splittable optical fiber ribbons|
|US9110265||Jun 17, 2013||Aug 18, 2015||Prysmian Communication Cables And Systems Usa, Llc||Splittable optical fiber ribbons|
|WO2008042171A2 *||Sep 25, 2007||Apr 10, 2008||Chiasson David W||Fiber optic ribbons having one or more predetermined fracture regions|
|WO2008042172A2 *||Sep 25, 2007||Apr 10, 2008||Corning Cable Sys Llc||Fiber optic ribbon subunits having ends with different shapes|
|International Classification||G02B, G02B6/44|
|Cooperative Classification||G02B6/4495, G02B6/4404|
|Apr 10, 2003||AS||Assignment|
Owner name: CORNING CABLE SYSTEMS LLC, NORTH CAROLINA
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:CONRAD, CRAIG M.;CHIASSON, DAVID W.;BLAZER, BRADLEY J.;AND OTHERS;REEL/FRAME:013981/0029;SIGNING DATES FROM 20030409 TO 20030410
|Feb 1, 2005||CC||Certificate of correction|
|Mar 10, 2008||FPAY||Fee payment|
Year of fee payment: 4
|Feb 27, 2012||FPAY||Fee payment|
Year of fee payment: 8
|Aug 25, 2014||AS||Assignment|
Owner name: CCS TECHNOLOGY, INC., DELAWARE
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:CORNING CABLE SYSTEMS LLC;REEL/FRAME:033600/0408
Effective date: 20030124
|Aug 28, 2014||AS||Assignment|
Owner name: CCS TECHNOLOGY, INC., DELAWARE
Free format text: CORRECTIVE ASSIGNMENT TO CORRECT THE EXECUTION DATE TO READ 04/27/2004 PREVIOUSLY RECORDED ON REEL 033600 FRAME 0408. ASSIGNOR(S) HEREBY CONFIRMS THE CORRECTION OF THE EXECUTION DATE TO READ 04/27/2004;ASSIGNOR:CORNING CABLE SYSTEMS LLC;REEL/FRAME:033646/0892
Effective date: 20040427